The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges /
| Main Author: | |
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| Corporate Authors: | , |
| Format: | Government Document eBook |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1952.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 2679. |
| Subjects: | |
| Online Access: | Connect to the full text of this electronic book |
Internet
Connect to the full text of this electronic bookAvailable Online
| Call Number: |
TA660.P6 |
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|---|---|---|
| Call Number | Status | Get It |
| TA660.P6 | Available | |